JPH02124800U - - Google Patents
Info
- Publication number
- JPH02124800U JPH02124800U JP3374389U JP3374389U JPH02124800U JP H02124800 U JPH02124800 U JP H02124800U JP 3374389 U JP3374389 U JP 3374389U JP 3374389 U JP3374389 U JP 3374389U JP H02124800 U JPH02124800 U JP H02124800U
- Authority
- JP
- Japan
- Prior art keywords
- bolt
- rocket
- catcher
- coil spring
- captures
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000926 separation method Methods 0.000 claims description 6
- 230000008878 coupling Effects 0.000 claims 2
- 238000010168 coupling process Methods 0.000 claims 2
- 238000005859 coupling reaction Methods 0.000 claims 2
- 238000010586 diagram Methods 0.000 description 2
Description
第１図は、この考案の実施例であり人工衛星と
ロケツトの分離前の形状図、第２図は、アームの
連結状態を示す外観図、第３図は、人工衛星とロ
ケツトの分離後の形状図、第４図は、従来の人工
衛星とロケツト分離後の形状図である。
図において、１はボルト、２はリテーナ、３は
キヤツチヤベース、４はアーム、５はコイルバネ
、Ｃはボルトキヤツチヤ、Ｎは分離ナツト、Ｒは
ロケツト、Ｓは人工衛星である。なお、図中同一
符号は同一又は相当部分を示す。
Fig. 1 shows an embodiment of this invention, and is a diagram of the shape of the satellite and rocket before separation, Fig. 2 is an external view showing the connected state of the arms, and Fig. 3 shows the shape of the satellite and rocket after separation. Figure 4 is a diagram showing the configuration of a conventional artificial satellite and a rocket after they have been separated. In the figure, 1 is a bolt, 2 is a retainer, 3 is a catch base, 4 is an arm, 5 is a coil spring, C is a bolt catcher, N is a separation nut, R is a rocket, and S is an artificial satellite. Note that the same reference numerals in the figures indicate the same or corresponding parts.
Claims (1)
り放出された結合ボルトを捕獲するボルトキヤツ
チヤにおいて、一端がロケツト側をヒンジとして
結合され、かつ他端が上記ボルトキヤツチヤのベ
ースに結合されたアームと、上記ヒンジに設けら
れ、その回転力により、分離ナツトの作動と同時
に結合ボルトを捕獲した上記ボルトキヤツチヤを
人工衛星側から解放しロケツト側へ移すコイルバ
ネとを具備したことを特徴とするボルトキヤツチ
ヤ。 A bolt catcher that captures a coupling bolt released by a separation nut at a separation part between an artificial satellite and a rocket, and an arm having one end coupled with the rocket side as a hinge and the other end coupled to the base of the bolt catcher. , a bolt catcher comprising: a coil spring provided on the hinge; the bolt catcher, which captures the coupling bolt at the same time as the separation nut is actuated, is released from the satellite side and transferred to the rocket side by the rotational force of the coil spring; Tsuchiya.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3374389U JPH02124800U (en) | 1989-03-24 | 1989-03-24 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3374389U JPH02124800U (en) | 1989-03-24 | 1989-03-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02124800U true JPH02124800U (en) | 1990-10-15 |
Family
ID=31537649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3374389U Pending JPH02124800U (en) | 1989-03-24 | 1989-03-24 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02124800U (en) |
-
1989
- 1989-03-24 JP JP3374389U patent/JPH02124800U/ja active Pending